CN211194729U - Novel injection molding machine aircraft nose reposition of redundant personnel core is dismantled device - Google Patents
Novel injection molding machine aircraft nose reposition of redundant personnel core is dismantled device Download PDFInfo
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- CN211194729U CN211194729U CN201921621603.8U CN201921621603U CN211194729U CN 211194729 U CN211194729 U CN 211194729U CN 201921621603 U CN201921621603 U CN 201921621603U CN 211194729 U CN211194729 U CN 211194729U
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- reposition
- core
- redundant personnel
- shunt
- screw rod
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- Expired - Fee Related
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Abstract
The utility model relates to a belong to electric wire and cable manufacture equipment technical field, in particular to novel injection molding machine aircraft nose reposition of redundant personnel core dismantlement device comprises travelling car, reposition of redundant personnel core loading portion, reposition of redundant personnel core separation portion, and reposition of redundant personnel core loading portion sets up on the travelling car, reposition of redundant personnel core separation portion sets up on reposition of redundant personnel core loading portion, reposition of redundant personnel core loading portion comprises assembly base, dustpan shape branch bracket, slide bar, slider, semi-circular reposition of redundant personnel core support groove, connecting screw, and the assembly base is adorned admittedly in the travelling car top surface, and the slide bar symmetry is adorned admittedly in assembly base both sides, and the slider symmetry slides and sets up on the slide bar, and dustpan shape bracket rear end middle part is adorned admittedly in reposition of redundant personnel core separation portion, and both sides and slider dustpan are adorned admittedly mutually, and semi-circular reposition of redundant personnel core support groove. The utility model discloses structural design scientific and reasonable has advantages such as dismantle convenient, labour saving and time saving, security height, application scope are wide, has higher novelty.
Description
Technical Field
The utility model belongs to the technical field of wire and cable manufacture equipment, in particular to novel injection molding machine aircraft nose reposition of redundant personnel core dismantlement device.
Background
The rubber electric wire and cable production line is characterized in that the product specifications are various, the length customization is carried out according to the requirements of customers, the product specifications are generally short, the rubber materials with different types and colors need to be frequently replaced, and the wire core specifications need to be replaced correspondingly. Each production line is usually only provided with one machine head (a single extrusion machine head is provided with one shunt core, a double-layer machine head is provided with four shunt cores, and a three-layer and double-layer common production line is provided with five shunt cores); however, when the rubber material in the shunt core of the machine head is cleaned or the shunt core and a machine head die are replaced, the shunt core must be pulled out from the shunt core, the production line worker traditionally operates in a mode that an ejection screw penetrates through a screw hole reserved on the shunt core and abuts against the end face of a machine head body, and the screw is manually rotated by a wrench to enable the shunt core and the machine head body to generate a gap.
Disclosure of Invention
An object of the utility model is to overcome the not enough of prior art, provide a simple structure, preparation are easy, convenient to use, labour saving and time saving, security are high, can dismantle reposition of redundant personnel core, effectively prolong reposition of redundant personnel core life's novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device fast.
The utility model provides a its technical problem realize through following technical scheme:
the utility model provides a novel injection molding machine aircraft nose reposition of redundant personnel core dismantlement device which characterized in that: the shunt core loading part is arranged on the moving trolley, the shunt core separating part is arranged on the shunt core loading part, the shunt core loading part is composed of an assembly base, a dustpan-shaped shunt bracket, a sliding bar, a sliding block, a semicircular shunt core supporting groove and a connecting screw rod, the assembly base is fixedly arranged on the top surface of the moving trolley, the sliding bar is symmetrically and fixedly arranged on two sides of the assembly base, the sliding block is symmetrically and slidably arranged on the sliding bar, the middle part of the rear end of the dustpan-shaped bracket is fixedly arranged on the shunt core separating part, two sides of the dustpan-shaped bracket are fixedly arranged with the sliding block, the semicircular shunt core supporting groove is fixedly arranged at the front end of the dustpan-shaped bracket, and the connecting screw rod is symmetrically connected between the semicircular shunt core supporting groove and the shunt core.
And the shunting core separating part consists of a hand wheel, a screw rod sleeve, a screw rod and a nut, wherein the screw rod sleeve is fixedly arranged at the rear end of the assembly base, the nut is fixedly arranged with the dustpan-shaped bracket, the screw rod is arranged in the screw rod sleeve and the nut, and the hand wheel is fixedly arranged at the outer end part of the screw rod.
Moreover, the semicircular shunt core bracket and the shunt core are correspondingly provided with various specifications.
And the top surface of the front end of the assembling base is symmetrically provided with cushion blocks.
The utility model discloses an advantage and beneficial effect do:
1. this novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device simple structure, the preparation is easy, convenient assembling.
2. This novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device is provided with reposition of redundant personnel core separation portion, reposition of redundant personnel core loading portion, dismantles reposition of redundant personnel core labour saving and time saving, and the security is high.
3. This novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device is provided with the travelling car, can conveniently transport the predetermined place with the reposition of redundant personnel core after the dismantlement.
4. This novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device is provided with the semi-circular reposition of redundant personnel core of multiple specification and holds in the palm the groove, and applicable in the dismantlement of multiple specification reposition of redundant personnel core, application scope is wide.
5. This novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device is when dismantling the reposition of redundant personnel core, and connecting screw is in relative quiescent condition with the reposition of redundant personnel core, and connecting screw that can significantly reduce wears with the reposition of redundant personnel core, effectively prolongs connecting screw and reposition of redundant personnel core life.
6. This novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device structural design scientific and reasonable has simple structure, the preparation is easy, dismantles advantages such as convenient, labour saving and time saving, security height, application scope are wide, is a novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device who has higher novelty.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of fig. 1.
1-a hand wheel, 2-an assembly base, 3-a screw rod sleeve, 4-a screw rod, 5-a nut, 6-a dustpan-shaped bracket, 7-a connecting screw rod, 8-a semicircular shunt core bracket, 9-a cushion block, 10-a movable trolley, 11-a shunt core, 12-a slide bar and 13-a slide block.
Detailed Description
The present invention will be described in further detail with reference to specific examples, which are provided for illustrative purposes only, and are not intended to be limiting, and the scope of the present invention should not be limited thereby.
The utility model provides a novel injection molding machine aircraft nose reposition of redundant personnel core dismounting device, comprises travelling car 10, reposition of redundant personnel core loading portion, reposition of redundant personnel core separation portion, and reposition of redundant personnel core loading portion sets up on the travelling car, and reposition of redundant personnel core separation portion sets up on reposition of redundant personnel core loading portion.
The shunt core loading part comprises an assembly base 2, a dustpan-shaped bracket 6, a sliding bar 12, a sliding block 13, a semicircular shunt core supporting groove 8 and a connecting screw 7, wherein the assembly base is fixedly arranged on the top surface of the movable trolley, the sliding bar is symmetrically and fixedly arranged on two sides of the assembly base, the sliding block is symmetrically and slidably arranged on the sliding bar, the middle part of the rear end of the dustpan-shaped bracket is fixedly arranged on a nut of the shunt core separating part, two sides of the dustpan-shaped bracket are fixedly arranged with the sliding block, the semicircular shunt core supporting groove is fixedly arranged at the front end of the dustpan-shaped bracket, and the connecting screw is symmetrically connected between the semicircular shunt core supporting groove. The semicircular shunt core bracket and the shunt core are correspondingly provided with various specifications. Cushion blocks 9 are symmetrically arranged on the top surface of the front end of the assembling base. The bracket with the semicircular shunt cores of various specifications can be suitable for disassembling shunt cores of different specifications; the arrangement of the cushion block can keep balance of the dustpan-shaped bracket, reduce friction between the dustpan-shaped bracket and the assembly base and reduce friction between the sliding block and the sliding bar.
The split-flow core separating part consists of a hand wheel 1, a screw rod sleeve 3, a screw rod 4 and a nut 5, the screw rod sleeve is fixedly arranged at the rear end of the assembling base, the nut and the dustpan-shaped bracket are fixedly arranged, the screw rod is arranged in the screw rod sleeve and the nut, and the hand wheel is fixedly arranged at the outer end part of the screw rod.
The utility model discloses a theory of operation does:
when the shunt core of the injection molding machine head needs to be disassembled, a semicircular shunt core support groove matched with the specification of the shunt core is selected and assembled firstly, then the movable trolley is pushed, the semicircular shunt core support groove is opposite to the shunt core, the hand wheel is rotated leftwards, the hand wheel drives the lead screw to rotate, under the action of the screw nut, the dustpan-shaped support moves forwards, the semicircular shunt core support groove supports the shunt core, and the connecting screw rod is connected with the shunt core in a rotating mode. And then the hand wheel is rotated rightwards, the hand wheel drives the screw rod to rotate, under the action of the screw nut, the dustpan-shaped bracket and the connecting screw rod move backwards and drive the shunting core to move backwards, and finally the shunting core is separated from the machine head of the injection molding machine. And then, pushing the moving trolley to transfer the shunt core to a preset position. And the shunt core is disassembled.
Although the embodiments of the present invention and the accompanying drawings are disclosed for illustrative purposes, those skilled in the art will appreciate that: various substitutions, changes and modifications are possible without departing from the spirit and scope of the present invention and the appended claims, and therefore, the scope of the present invention is not limited to the disclosure of the embodiments and the accompanying drawings.
Claims (4)
1. The utility model provides a novel injection molding machine aircraft nose reposition of redundant personnel core dismantlement device which characterized in that: the shunt core loading part is arranged on the moving trolley, the shunt core separating part is arranged on the shunt core loading part, the shunt core loading part is composed of an assembly base, a dustpan-shaped shunt bracket, a sliding bar, a sliding block, a semicircular shunt core supporting groove and a connecting screw rod, the assembly base is fixedly arranged on the top surface of the moving trolley, the sliding bar is symmetrically and fixedly arranged on two sides of the assembly base, the sliding block is symmetrically and slidably arranged on the sliding bar, the middle part of the rear end of the dustpan-shaped bracket is fixedly arranged on the shunt core separating part, two sides of the dustpan-shaped bracket are fixedly arranged with the sliding block, the semicircular shunt core supporting groove is fixedly arranged at the front end of the dustpan-shaped bracket, and the connecting screw rod is symmetrically connected between the semicircular shunt core supporting groove and the shunt core.
2. The novel dismounting device for the machine head shunt core of the injection molding machine as claimed in claim 1, is characterized in that: the split-flow core separating part consists of a hand wheel, a screw rod sleeve, a screw rod and a nut, the screw rod sleeve is fixedly arranged at the rear end of the assembling base, the nut is fixedly arranged with the dustpan-shaped bracket, the screw rod is arranged in the screw rod sleeve and the nut, and the hand wheel is fixedly arranged at the outer end part of the screw rod.
3. The novel dismounting device for the machine head shunt core of the injection molding machine as claimed in claim 1, is characterized in that: the semicircular shunt core bracket and the shunt core are correspondingly provided with various specifications.
4. The novel dismounting device for the machine head shunt core of the injection molding machine as claimed in claim 1, is characterized in that: cushion blocks are symmetrically arranged on the top face of the front end of the assembling base.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921621603.8U CN211194729U (en) | 2019-09-26 | 2019-09-26 | Novel injection molding machine aircraft nose reposition of redundant personnel core is dismantled device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921621603.8U CN211194729U (en) | 2019-09-26 | 2019-09-26 | Novel injection molding machine aircraft nose reposition of redundant personnel core is dismantled device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN211194729U true CN211194729U (en) | 2020-08-07 |
Family
ID=71884939
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201921621603.8U Expired - Fee Related CN211194729U (en) | 2019-09-26 | 2019-09-26 | Novel injection molding machine aircraft nose reposition of redundant personnel core is dismantled device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN211194729U (en) |
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2019
- 2019-09-26 CN CN201921621603.8U patent/CN211194729U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200807 |
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CF01 | Termination of patent right due to non-payment of annual fee |